SPACE ENVIRONMENTS SEMINAR—PART II
The second AIAA space environments seminar will focus on Spacecraft Charging and the effects of Micrometeroids and Space Debris. Each of these interactions are discussed below.
Spacecraft Charging: Spacecraft Charging is caused by the interaction of charged particles with external spacecraft surfaces (surface charging) and, in the case of internal charging, with the buildup of charge in and on dielectrics and surfaces within the vehicle. The buildup of charge can affect particle measurements or can lead to arcing between surfaces or breakdown in dielectrics. The talk will review briefly the environments that can cause significant charging, develop the equations for surface and internal charging, review the effects of arcing, and discuss the methods for limiting charging effects with emphasis on the NASA 4002 series of guidelines.
Micrometeroids and Space Debris: Micrometeroid and space debris impacts on space vehicles can of course cause significant damage and even destroy them. Returned surfaces from Earth-orbiting spacecraft have often provided examples of pitting and indeed the windows on the Space Shuttle have shown cracks due to impacts. In this talk, following a review of the ambient meteoroid environment and the growing space debris environment at Earth, we will review the equations for computing the effects of hypervelocity impacts. These will be divided into single surface and double surfaces (e.g., Whipple shields). Methods such as the Whipple shield for protecting spacecraft and the computations necessary to evaluate an overall meteoroid shielding design will be presented.
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